From: Effects of aspect ratio and inclination angle on aerodynamic loads of a flat plate
Experiments | Aspect Ratio (AR) | Thickness/Chord | Reynolds (based on chord length and inlet velocity) | Inclination angle |
---|---|---|---|---|
Fage and Johansen [1] | 14.1 (infinite) | 0.03 | 150,000 | 0.15° ~ 90° |
12° ~ 90° | ||||
Flaschbart [2] | 50 ~ 200 | 0.015 ~ 0.05 | 1000 ~ 6000 | 90° |
Schubauer and Dryden [3] | 6 | – | 30,000 ~ 60,000 | 90° |
Roshko [4] | 13.5 | 0.16 | 4000 ~ 10,000 | 90° |
Arie and Rouse [5] | 12 | 0.083 | 75,000 | 90° |
Fail, Lawford and Eyre [6] | 1 ~ 20 | – | 80,000 | 90° |
Abernathy [7] | 1.5 ~ 6 | 0.06 ~ 0.19 | 36,000 ~ 140,000 | 40° ~ 90° |
Castro [8] | 15 | 0.04 | 25,000 ~ 90,000 | 90° |
Sarpkaya & Kline [9] | 8 | 0.11 | 21,000 | 90° |
Kiya and Matsumura [10] | 15 | 0.215 | 23,000 | 90° |
Mazharoglu and Hacisevki [11] | 14 | 0.2 | 33,000 | 90° |
Xu et al. [12] | 12.1 | 0.125 | 2240 | 90° |